An Investigation of Aerodynamic Heating to Spherically Blunted Cones at Angle of Attack

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ISBN 13 :
Total Pages : 240 pages
Book Rating : 4.:/5 (269 download)

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Book Synopsis An Investigation of Aerodynamic Heating to Spherically Blunted Cones at Angle of Attack by : Jason Paul Shimshi

Download or read book An Investigation of Aerodynamic Heating to Spherically Blunted Cones at Angle of Attack written by Jason Paul Shimshi and published by . This book was released on 1992 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Real-gas Effects on the Aerodynamics of Blunt Cones as Measured in a Hypervelocity Range

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Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Real-gas Effects on the Aerodynamics of Blunt Cones as Measured in a Hypervelocity Range by : C. J. Welsh

Download or read book Real-gas Effects on the Aerodynamics of Blunt Cones as Measured in a Hypervelocity Range written by C. J. Welsh and published by . This book was released on 1979 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow by : David E. Boylan

Download or read book Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow written by David E. Boylan and published by . This book was released on 1973 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg in a low-density, hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author).

Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ by : Dennis M. Bushnell

Download or read book Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ written by Dennis M. Bushnell and published by . This book was released on 1968 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of Spherically Blunted Cones at Mach Numbers from 0.5 to 5.0

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Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Characteristics of Spherically Blunted Cones at Mach Numbers from 0.5 to 5.0 by : Robert V. Owens

Download or read book Aerodynamic Characteristics of Spherically Blunted Cones at Mach Numbers from 0.5 to 5.0 written by Robert V. Owens and published by . This book was released on 1965 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 by : Jerome D. Julius

Download or read book Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 written by Jerome D. Julius and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Transonic Investigation of the Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Base Shape on the Static Aerodynamic Characteristics of Short, Blunt Cones at Angles of Attack to 1800

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ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Transonic Investigation of the Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Base Shape on the Static Aerodynamic Characteristics of Short, Blunt Cones at Angles of Attack to 1800 by : Cuyler W. Brooks

Download or read book Transonic Investigation of the Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Base Shape on the Static Aerodynamic Characteristics of Short, Blunt Cones at Angles of Attack to 1800 written by Cuyler W. Brooks and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone Cylinder at Hypersonic Free Flight Mach Numbers Up to 20.4

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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone Cylinder at Hypersonic Free Flight Mach Numbers Up to 20.4 by :

Download or read book Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone Cylinder at Hypersonic Free Flight Mach Numbers Up to 20.4 written by and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Study of Laminar Heat Transfer to Spherically Blunted Cones and Hemisphere-cylinders at Hypersonic Conditions

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Study of Laminar Heat Transfer to Spherically Blunted Cones and Hemisphere-cylinders at Hypersonic Conditions by : B. J. Griffith

Download or read book A Study of Laminar Heat Transfer to Spherically Blunted Cones and Hemisphere-cylinders at Hypersonic Conditions written by B. J. Griffith and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone During Free Flight at Mach Numbers Up to 20.8

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone During Free Flight at Mach Numbers Up to 20.8 by :

Download or read book Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone During Free Flight at Mach Numbers Up to 20.8 written by and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Heating on the Corrugated Surface of a 10.20 Half-angle Blunted Cone at Mach 6.7

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Heating on the Corrugated Surface of a 10.20 Half-angle Blunted Cone at Mach 6.7 by : Irving Weinstein

Download or read book Aerodynamic Heating on the Corrugated Surface of a 10.20 Half-angle Blunted Cone at Mach 6.7 written by Irving Weinstein and published by . This book was released on 1981 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90°

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° by : Raul Jorge Conti

Download or read book Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° written by Raul Jorge Conti and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two circulation conical configurations having 15° half-angles were tested in laminar boundary layer at a Mach number of 6 and angles of attack up to 90°. One cone had a sharp nose and a fineness ratio of 1.87 and the other had a spherically blunted nose with a bluntness ratio of 0.1428 and a fineness ratio of 1.66. Pressure measurements and schlieren pictures of the flow showed that near-conical flow existed above 70° high pressure areas were present near the base and the bow shock wave was considerably curved.

Aerodynamic Characteristics of a Spherically Blunted 25° Cone at a Mach Number of 20

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Characteristics of a Spherically Blunted 25° Cone at a Mach Number of 20 by : Julius E. Harris

Download or read book Aerodynamic Characteristics of a Spherically Blunted 25° Cone at a Mach Number of 20 written by Julius E. Harris and published by . This book was released on 1967 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Super- and Hypersonic Aerodynamics and Heat Transfer

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Publisher : Routledge
ISBN 13 : 1351412930
Total Pages : 209 pages
Book Rating : 4.3/5 (514 download)

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Book Synopsis Super- and Hypersonic Aerodynamics and Heat Transfer by : V.Z. Parton

Download or read book Super- and Hypersonic Aerodynamics and Heat Transfer written by V.Z. Parton and published by Routledge. This book was released on 2018-03-29 with total page 209 pages. Available in PDF, EPUB and Kindle. Book excerpt: Recent government and commercial efforts to develop orbital and suborbital passenger and transport aircraft have resulted in a burgeoning of new research. The articles in this book, translated from Russian, were contributed by the world's leading authorities on supersonic and hypersonic flows and heat transfer. This superb book addresses the physics and engineering aspects of ultra high-speed aerodynamic problems. Thorough coverage is given to an array of specific problem-solving equations. Super- and Hypersonic Aerodynamics and Heat Transfer will be essential reading for all aeronautical engineers, mechanical engineers, mathematicians, and physicists involved in this exciting field of research.

A Simplified Method for Calculating Laminar Heat Transfer Over Bodies at an Angle of Attack

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Simplified Method for Calculating Laminar Heat Transfer Over Bodies at an Angle of Attack by : Fred R. DeJarnette

Download or read book A Simplified Method for Calculating Laminar Heat Transfer Over Bodies at an Angle of Attack written by Fred R. DeJarnette and published by . This book was released on 1968 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone by : William R. Wehrend

Download or read book Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone written by William R. Wehrend and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Investigation for the Aerodynamic and Heat Transfer Characteristics of Slender Hypersonic Cones Over a Wide Range of Angles of Attack

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ISBN 13 :
Total Pages : 133 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis The Investigation for the Aerodynamic and Heat Transfer Characteristics of Slender Hypersonic Cones Over a Wide Range of Angles of Attack by : Paul K. Chang

Download or read book The Investigation for the Aerodynamic and Heat Transfer Characteristics of Slender Hypersonic Cones Over a Wide Range of Angles of Attack written by Paul K. Chang and published by . This book was released on 1971 with total page 133 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problems of aerodynamic and heat transfer characteristics of slender sharp nosed hypersonic cones over a wide range of angles of attack are examined and the analytical solutions are presented. Three particular problems are studied: (1) inviscid flow characteristics of shock layer involving laminar separation in the leeward side with undisturbed free stream Mach number 7.95 and angle of attack 20 degrees for cone half angle 10 degrees, (2) attached three-dimensional compressible boundary layer over the cone, (3) aerodynamic and heat transfer characteristics of turbulent separated flow. (Author).